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RLG INS Navigation System Modulated Inertial System For Military Vehicles

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Miss. Yao

yao@inertial-systems.com

86--18771146215-13212796772

13212796772

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RLG INS Navigation System Modulated Inertial System For Military Vehicles

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 sets per year

Details Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Accelerometer/Months Bias Repeatability（1σ）:

≤20μg

Accelerometer/Months Scale Factor Accuracy（1σ）:

≤20ppm

Gyro/Bias Repeatability（1σ）:

≤0.01°/hr,1σ

Gyro/Scale Factor Accuracy（1σ）:

≤5ppm

Gyro/Random Walk（1σ）:

≤0.003°/√hr

Angular Rate:

≥±400°/sec

Angular Acceleration:

100000°/sec2

Acceleration:

＞25g

Angular Attitude:

Any Orientation

Alignment Time:

≤15min

Input/output:

3 RS422 Full-duplex Serial Ports, 1 100M Ethernet Port

Position Accuracy/10min Zero Speed Correction:

≤5m

Position Accuracy/Inertial Navigation/odometer Combination:

≤0.08%D

Position Accuracy/North Finding/orientation Accuracy:

≤0.4mil

Position Accuracy/Bearing Keeping Accuracy Per 2h:

≤0.4mil

Position Accuracy/Combined Navigation Position Accuracy:

≤0.2mil

AHRS Applications Performance/Heading Accuracy:

≤0.2mil

AHRS Applications Performance/Pitch & Roll Accuracy:

≤0.2mil

Power Consumption:

＜40W

Dimensions:

Weight:

＜6.5kg

Temperature:

-40℃~60℃

Shock:

15g，Half-sine Wave 11ms

Input Voltage:

DC24V(±25%)

Cooling:

Conduction To Mounting Plate

Vibration:

20~2000Hz,6.06g

MTBF:

＞15000 Hours

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Strapdown ins navigation system

military vehicles ins navigation system

military vehicles strapdown inertial system

Product Description

Our advanced Land RLG INS integrates precision optical gyros (RLG/FOG) and quartz accelerometers within a rugged strapdown architecture, delivering accurate and reliable navigation data for ground vehicles. The system supports flexible operational modes, including zero-velocity updates (ZUPT) and multi-sensor fusion, ensuring consistent performance even in GNSS-denied or challenging environments.

Applications:

Military combat and armored vehicles
Unmanned ground vehicles (UGVs)
Agricultural and industrial equipment
Special-purpose autonomous land platforms

Key Advantages:

Versatile initialization and alignment options for rapid deployment
Reliable navigation in GNSS-denied or degraded conditions
Robust operation in extreme environments with vibration, shock, and temperature resilience
Battle-tested reliability for mission-critical operations

Series		Land Inertial Navigation System(INS-L)
Accelerometer	Months Bias Repeatability(1σ)	≤20μg
Accelerometer	Months Scale Factor Accuracy(1σ)	≤20ppm
Gyro	Bias Repeatability(1σ)	≤0.01°/h
	Scale Factor Accuracy(1σ)	≤5ppm
	Random walk(1σ)	≤0.003°/√hr
Features	Angular Rate	≥±400°/sec
	Angular Acceleration	100000°/sec2
	Acceleration	＞25g
	Angular Attitude	Any Orientation
	Alignment time	≤15min
	Input/output	3 RS422 full-duplex serial ports, 1 100M Ethernet port
Position accuracy	10min zero speed correction	≤5m
	Inertial navigation/odometer combination	≤0.08%D
	North finding/orientation accuracy	≤0.4mil
	Bearing keeping accuracy/2h	≤0.4mil
	Combined navigation position accuracy	≤0.2mil
AHRS Applications Performance	Heading Accuracy	≤0.2mil
AHRS Applications Performance	Pitch & Roll Accuracy	≤0.2mil
Characteristics	Power consumption	＜40W
	Dimensions	--
	Weight	＜6.5kg
	Temperature	-40℃~60℃
	Shock	15g,Half-sine wave 11ms
	Input Voltage	DC24V(±25%)
	cooling	Conduction to mounting plate
	Vibration	20~2000Hz,6.06g
	MTBF	＞15000 hours

Tags:

strapdown inertial system,

inu inertial navigation unit,

inertial guidance system

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PRODUCTS DETAILS

Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

RLG INS Navigation System Modulated Inertial System For Military Vehicles

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 sets per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Accelerometer/Months Bias Repeatability（1σ）:

≤20μg

Accelerometer/Months Scale Factor Accuracy（1σ）:

≤20ppm

Gyro/Bias Repeatability（1σ）:

≤0.01°/hr,1σ

Gyro/Scale Factor Accuracy（1σ）:

≤5ppm

Gyro/Random Walk（1σ）:

≤0.003°/√hr

Angular Rate:

≥±400°/sec

Angular Acceleration:

100000°/sec2

Acceleration:

＞25g

Angular Attitude:

Any Orientation

Alignment Time:

≤15min

Input/output:

3 RS422 Full-duplex Serial Ports, 1 100M Ethernet Port

Position Accuracy/10min Zero Speed Correction:

≤5m

Position Accuracy/Inertial Navigation/odometer Combination:

≤0.08%D

Position Accuracy/North Finding/orientation Accuracy:

≤0.4mil

Position Accuracy/Bearing Keeping Accuracy Per 2h:

≤0.4mil

Position Accuracy/Combined Navigation Position Accuracy:

≤0.2mil

AHRS Applications Performance/Heading Accuracy:

≤0.2mil

AHRS Applications Performance/Pitch & Roll Accuracy:

≤0.2mil

Power Consumption:

＜40W

Dimensions:

Weight:

＜6.5kg

Temperature:

-40℃~60℃

Shock:

15g，Half-sine Wave 11ms

Input Voltage:

DC24V(±25%)

Cooling:

Conduction To Mounting Plate

Vibration:

20~2000Hz,6.06g

MTBF:

＞15000 Hours

Minimum Order Quantity:

1 set

Price:

$1000-$100000

Delivery Time:

30 work days

Payment Terms:

T/T

Supply Ability:

500 sets per year

Highlight

Strapdown ins navigation system

military vehicles ins navigation system

military vehicles strapdown inertial system

Product Description

Applications:

Military combat and armored vehicles
Unmanned ground vehicles (UGVs)
Agricultural and industrial equipment
Special-purpose autonomous land platforms

Key Advantages:

Versatile initialization and alignment options for rapid deployment
Reliable navigation in GNSS-denied or degraded conditions
Robust operation in extreme environments with vibration, shock, and temperature resilience
Battle-tested reliability for mission-critical operations

Series		Land Inertial Navigation System(INS-L)
Accelerometer	Months Bias Repeatability(1σ)	≤20μg
Accelerometer	Months Scale Factor Accuracy(1σ)	≤20ppm
Gyro	Bias Repeatability(1σ)	≤0.01°/h
	Scale Factor Accuracy(1σ)	≤5ppm
	Random walk(1σ)	≤0.003°/√hr
Features	Angular Rate	≥±400°/sec
	Angular Acceleration	100000°/sec2
	Acceleration	＞25g
	Angular Attitude	Any Orientation
	Alignment time	≤15min
	Input/output	3 RS422 full-duplex serial ports, 1 100M Ethernet port
Position accuracy	10min zero speed correction	≤5m
	Inertial navigation/odometer combination	≤0.08%D
	North finding/orientation accuracy	≤0.4mil
	Bearing keeping accuracy/2h	≤0.4mil
	Combined navigation position accuracy	≤0.2mil
AHRS Applications Performance	Heading Accuracy	≤0.2mil
AHRS Applications Performance	Pitch & Roll Accuracy	≤0.2mil
Characteristics	Power consumption	＜40W
	Dimensions	--
	Weight	＜6.5kg
	Temperature	-40℃~60℃
	Shock	15g,Half-sine wave 11ms
	Input Voltage	DC24V(±25%)
	cooling	Conduction to mounting plate
	Vibration	20~2000Hz,6.06g
	MTBF	＞15000 hours

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